Patent GB-892483-A (GB)
Title: Thrust reverser for jet propulsion engines
IPC: F02K1/72
Filed: 1960-08-30
Abstract: 892,483. Jet propulsion engines thrust reversals. BOEING AIRPLANE CO. Aug. 30, 1960 [Sept. 8, 1959], No. 29931/60. Class 4. A jet propulsion engine has a discharge duct defined by inner and outer walls, the latter having a longitudinally movable section with an inner surface inclined to the direction of discharge, the inner wall being similarly inclined, so that the gas duct pressure exerts a forward force on the. section, means to move the section fore-and-aft to open and close a side opening in the outer wall, deflector means pivotally mounted on one wall to swing from a retracted position parallel to the wall to an extended position across the duct rearward of the opening to deflect gases outwardly and forwardly therethrough, actuator means pivotally connected to the deflector means, and means including linkage pivotally interconnecting the movable section and deflector means, to effect conjoint rearward movement of the movable section and deflector means followed by pivotal extension movement of the deflector means. The invention is applicable to an annular gas turbine exhaust nozzle, and to an annular bypass duct as shown in Figs. 3, 4, 7, and 8, where an annular section 14b of the outer wall of the by-pass duct defined by walls 14, 16, is movable downstream as shown in Figs. 7 and 8, to form an opening P. In the forward thrust position, Fig. 3, a rubber seal 15 on section 14b abuts a flange 14c<SP>1</SP> on the fixed wall 14c, and is inflated by the duct gas pressure through apertures 17. The section 14b has arms 32, one shown in Fig. 4, at circumferentially spaced positions, each arm having two sets of rollers 34 engaging both sides of a double sided guide track 26 secured to fixed structure. Co-operating stops 36, 38, limit the rearward movement of section 14b. Between each pair of adjacent guide tracks is located a curved deflector panel 40, Fig. 3, pivoted to the piston rod 62 of a jack 60 pivoted to fixed structure at 61. A link 52 is pivoted at 50 to a flange 40d on the deflector panel and, to the section 14b on a shaft 54. Adjacent shafts 54 may be connected by sector gears, Fig. 5 (not shown), to ensure synchronization of extension of the panels 40, and to permit one jack 60 to operate several deflector panels. Flanges on the sides of the deflector panels are connected to rollers 67 working in the guide tracks 26, Fig. 4. In the position of Fig. 3, one end 40a of each deflector panel rests on a collar 44 on wall 14c, and stops 52a, 70, on link 52 and section 14b, abut. The inclination of the opposed surfaces 14a, 16a, causes the gas pressure in the duct to exert a forward force on section 14b to maintain it in the position of Figs. 3, should the jacks 60 fail. On extension of the jacks, section 14b is moved to the position in Fig. 7. The toggles constituted by the deflector panels 40 and links 52, do not break during this movement, because of pressure of the gas-stream on the panels. Once the stops 36 and 38, Fig. 4, abut, however, further extension of the jacks overcomes the pressure on panels 40, and moves them to the position shown in Fig. 8. In this position the gas stream exerts a force on the deflector panels tending to maintain the position if the jacks 60 fail. The side edges of the deflector plates abut in this position, to prevent any gas flow rearwardly, and flanges 40b on the panels contact seal 15. On retraction of the jacks, the panels 40 first move outwardly until stops 52a and 70 abut, and section 14b is then moved to close opening P. In a modification, Figs. 9 to 11 (not shown), a guide vane is spaced from and fixed to each deflector panel, and the rearward edge of each vane rests on roller 44, which is extended rearwardly so that the deflector panel cannot move inwardly until the rearward movement of section 14b is substantially completed. In a further arrangement, Fig. 16, having a longer annular by-pass duct, forward discharge takes place well upstream of the discharge nozzle, and the opening in the outer wall is made by longitudinal movement of an annular section 208 and by opening a door 204 opposite each deflector panel 218. The doors 204 are opened by rotation about pivots 230 by links 232 pivoted at 234 to the arms 32, Fig. 4. An annular seal 224 is provided for section 208.